Active Control of a UAV Helicopter with a Slung Load for Precision Airborne Cargo Delivery

VFS-F66-000442

5/11/2010

Authors
Abstract
Content

An active controller for a UAV helicopter carrying a slung load is described in this paper. The objective of the controller is to allow the UAV to safely transport a slung load and to place it precisely on a moving ground platform such as a moving truck or a ship. In order to fulfill this objective, the active controller is synthesized in terms of three sub-components; first a target position tracker which generates position tracking commands, second a load oscillation controller which generates load oscillation damping commands, and third an adaptive neural network which compensates for uncertainties associated with flight environment and/or modeling errors. A linear PD controller is used for the target position tracking control. A nonlinear controller based on feedback linearization of the slung load dynamics is used for the load oscillation control. A single hidden layer neural network with an adaptive gain update is used for uncertainty compensation. The proposed controller is evaluated in simulations within the Georgia Tech UAV Simulation Tool (GUST) and in flight tests using the GTMax UAV helicopter testbed. Both simulation and flight test results are presented to demonstrate the effectiveness of the proposed controller in dampening of load oscillations while simultaneously reducing position errors relative to a virtual moving ground platform, in the presence of random ground vehicle motion, wind gusts and modeling errors.

Meta TagsDetails
DOI
https://doi.org/10.4050/VFS-F66-000442
Citation
Kang, K., Ottander, J., Prasad, J., and Johnson, E., "Active Control of a UAV Helicopter with a Slung Load for Precision Airborne Cargo Delivery," Forum 66 - Phoenix, AZ 2010, Phoenix, AZ, May 11, 2010, https://doi.org/10.4050/VFS-F66-000442.
Additional Details
Publisher
Published
5/11/2010
Product Code
VFS-F66-000442
Content Type
Technical Paper
Language
English